FR2552860B1 - Chambre de combustion chemisee - Google Patents

Chambre de combustion chemisee

Info

Publication number
FR2552860B1
FR2552860B1 FR8415112A FR8415112A FR2552860B1 FR 2552860 B1 FR2552860 B1 FR 2552860B1 FR 8415112 A FR8415112 A FR 8415112A FR 8415112 A FR8415112 A FR 8415112A FR 2552860 B1 FR2552860 B1 FR 2552860B1
Authority
FR
France
Prior art keywords
shirt
combustion chamber
combustion
chamber
shirt combustion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
FR8415112A
Other languages
English (en)
Other versions
FR2552860A1 (fr
Inventor
Thomas Lloyd Scott
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of FR2552860A1 publication Critical patent/FR2552860A1/fr
Application granted granted Critical
Publication of FR2552860B1 publication Critical patent/FR2552860B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/201—Heat transfer, e.g. cooling by impingement of a fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR8415112A 1983-10-03 1984-10-02 Chambre de combustion chemisee Expired FR2552860B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/538,302 US4567730A (en) 1983-10-03 1983-10-03 Shielded combustor

Publications (2)

Publication Number Publication Date
FR2552860A1 FR2552860A1 (fr) 1985-04-05
FR2552860B1 true FR2552860B1 (fr) 1988-10-28

Family

ID=24146336

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8415112A Expired FR2552860B1 (fr) 1983-10-03 1984-10-02 Chambre de combustion chemisee

Country Status (7)

Country Link
US (1) US4567730A (fr)
JP (1) JPS60111819A (fr)
CA (1) CA1217945A (fr)
DE (1) DE3435611A1 (fr)
FR (1) FR2552860B1 (fr)
GB (1) GB2147406B (fr)
IT (1) IT1176775B (fr)

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US5291732A (en) * 1993-02-08 1994-03-08 General Electric Company Combustor liner support assembly
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US5461866A (en) * 1994-12-15 1995-10-31 United Technologies Corporation Gas turbine engine combustion liner float wall cooling arrangement
GB9505067D0 (en) * 1995-03-14 1995-05-03 Europ Gas Turbines Ltd Combustor and operating method for gas or liquid-fuelled turbine
DE19547703C2 (de) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Brennkammer, insbesondere Ringbrennkammer, für Gasturbinentriebwerke
FR2752916B1 (fr) * 1996-09-05 1998-10-02 Snecma Chemise de protection thermique pour chambre de combustion de turboreacteur
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US6045134A (en) * 1998-02-04 2000-04-04 General Electric Co. Combined labyrinth and brush seals for rotary machines
US6139018A (en) * 1998-03-25 2000-10-31 General Electric Co. Positive pressure-actuated brush seal
US6047539A (en) * 1998-04-30 2000-04-11 General Electric Company Method of protecting gas turbine combustor components against water erosion and hot corrosion
US6168162B1 (en) 1998-08-05 2001-01-02 General Electric Co. Self-centering brush seal
US6250640B1 (en) 1998-08-17 2001-06-26 General Electric Co. Brush seals for steam turbine applications
ITMI991207A1 (it) * 1999-05-31 2000-12-01 Nuovo Pignone Spa Camera di combustione per turbine a gas
US6290232B1 (en) 1999-11-16 2001-09-18 General Electric Co. Rub-tolerant brush seal for turbine rotors and methods of installation
US6331006B1 (en) 2000-01-25 2001-12-18 General Electric Company Brush seal mounting in supporting groove using flat spring with bifurcated end
EP1152189A1 (fr) * 2000-05-05 2001-11-07 Siemens Aktiengesellschaft Procédé de protection d'un revêtement de SiO2 et appareil de combustion muni d'une telle protection
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FR2910115B1 (fr) * 2006-12-19 2012-11-16 Snecma Deflecteur pour fond de chambre de combustion, chambre de combustion en etant equipee et turboreacteur les comportant
US7726131B2 (en) * 2006-12-19 2010-06-01 Pratt & Whitney Canada Corp. Floatwall dilution hole cooling
FR2918443B1 (fr) * 2007-07-04 2009-10-30 Snecma Sa Chambre de combustion comportant des deflecteurs de protection thermique de fond de chambre et moteur a turbine a gaz en etant equipe
US8673234B2 (en) * 2008-03-04 2014-03-18 Aerojet Rocketdyne Of De, Inc. Reactor vessel and liner
US9052116B2 (en) * 2008-10-30 2015-06-09 Power Generation Technologies Development Fund, L.P. Toroidal heat exchanger
US9074005B2 (en) * 2009-01-02 2015-07-07 Washington State University Compositions and methods for modulating plant disease resistance and immunity
JP5320177B2 (ja) * 2009-06-18 2013-10-23 川崎重工業株式会社 ガスタービン燃焼器
DE102009035550A1 (de) * 2009-07-31 2011-02-03 Man Diesel & Turbo Se Gasturbinenbrennkammer
EP2428647B1 (fr) * 2010-09-08 2018-07-11 Ansaldo Energia IP UK Limited Zone de transition pour une chambre de combustion d'une turbine à gaz
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US9534783B2 (en) 2011-07-21 2017-01-03 United Technologies Corporation Insert adjacent to a heat shield element for a gas turbine engine combustor
JP5821550B2 (ja) * 2011-11-10 2015-11-24 株式会社Ihi 燃焼器ライナ
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JP6162949B2 (ja) * 2011-12-16 2017-07-12 ゼネラル・エレクトリック・カンパニイ Ｃｍｃライナの強化冷却のための一体化バッフルシステム
US9353948B2 (en) 2011-12-22 2016-05-31 General Electric Company Gas turbine combustor including a coating having reflective characteristics for radiation heat and method for improved combustor temperature uniformity
DE102012213637A1 (de) * 2012-08-02 2014-02-06 Siemens Aktiengesellschaft Brennkammerkühlung
EP2900970B1 (fr) * 2012-09-30 2018-12-05 United Technologies Corporation Écran thermique d'interface pour une chambre de combustion d'un moteur à turbine à gaz
US10088162B2 (en) 2012-10-01 2018-10-02 United Technologies Corporation Combustor with grommet having projecting lip
WO2014163669A1 (fr) * 2013-03-13 2014-10-09 Rolls-Royce Corporation Ensemble chambre de combustion pour turbine à gaz
US9651258B2 (en) 2013-03-15 2017-05-16 Rolls-Royce Corporation Shell and tiled liner arrangement for a combustor
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WO2015038293A1 (fr) * 2013-09-11 2015-03-19 United Technologies Corporation Chemise de chambre de combustion
JP6228685B2 (ja) 2013-09-11 2017-11-08 ゼネラル・エレクトリック・カンパニイ ばねで荷重されシールされるセラミックマトリックス複合材燃焼器ライナ
JP6202976B2 (ja) * 2013-10-10 2017-09-27 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
CN103557536B (zh) * 2013-11-14 2016-01-06 深圳智慧能源技术有限公司 陶瓷热屏蔽片及耐热结构
US10794595B2 (en) * 2014-02-03 2020-10-06 Raytheon Technologies Corporation Stepped heat shield for a turbine engine combustor
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US10830448B2 (en) * 2016-10-26 2020-11-10 Raytheon Technologies Corporation Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustor
US10739001B2 (en) * 2017-02-14 2020-08-11 Raytheon Technologies Corporation Combustor liner panel shell interface for a gas turbine engine combustor
US10823411B2 (en) 2017-02-23 2020-11-03 Raytheon Technologies Corporation Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor
US10830434B2 (en) 2017-02-23 2020-11-10 Raytheon Technologies Corporation Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
US10718521B2 (en) 2017-02-23 2020-07-21 Raytheon Technologies Corporation Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor
US10677462B2 (en) 2017-02-23 2020-06-09 Raytheon Technologies Corporation Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor
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Also Published As

Publication number Publication date
IT1176775B (it) 1987-08-18
DE3435611A1 (de) 1985-04-18
GB2147406B (en) 1987-02-25
FR2552860A1 (fr) 1985-04-05
CA1217945A (fr) 1987-02-17
IT8422791A0 (it) 1984-09-24
US4567730A (en) 1986-02-04
IT8422791A1 (it) 1986-03-24
GB2147406A (en) 1985-05-09
GB8422471D0 (en) 1984-10-10
JPS60111819A (ja) 1985-06-18

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